Navy plans to make jet fuel from sea water

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Nydoc
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Joined: Sat Nov 01, 2008 9:45 am

Post by Nydoc »

Joseph Chikva wrote:And ok, for providing you idea I've recalled who in Russia produces water electrolezers.
http://ekb.ru/products/119?action=small
Electrolizer producing 2.5 nm3/h of hydrogen without auxiliary hardware has dimensions 1.5 x 1.065 x 2.145 m
Total system volume 9.22 m3
Like numbers? :)
The site you linked actually lists the production rate minimum as 2.5 Nm3/h and maximum rate as 20 Nm3/h. In any case, the U.S.S. Nimitz can carry about 3.5 million gallons of JP-5. That is about 13250 cubic meters. Assuming a modern naval powerplant can produce 485MW and it was possible to use all that power at 4.9kWh/Nm3 of hydrogen, you could then fill a 3.5 million gallon tank with hydrogen in about 8 minutes. Four of your Russian units could fill it in a week.

sources:
http://www.fas.org/man//gao/nsiad98001/c1.htm
http://www.gastec.com.my/Hydrogen/H2%20 ... tation.pdf

Joseph Chikva
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Joined: Sat Apr 02, 2011 4:30 am

Post by Joseph Chikva »

Nydoc wrote:
Joseph Chikva wrote:And ok, for providing you idea I've recalled who in Russia produces water electrolezers.
http://ekb.ru/products/119?action=small
Electrolizer producing 2.5 nm3/h of hydrogen without auxiliary hardware has dimensions 1.5 x 1.065 x 2.145 m
Total system volume 9.22 m3
Like numbers? :)
The site you linked actually lists the production rate minimum as 2.5 Nm3/h and maximum rate as 20 Nm3/h. In any case, the U.S.S. Nimitz can carry about 3.5 million gallons of JP-5. That is about 13250 cubic meters. Assuming a modern naval powerplant can produce 485MW and it was possible to use all that power at 4.9kWh/Nm3 of hydrogen, you could then fill a 3.5 million gallon tank with hydrogen in about 8 minutes. Four of your units could fill it in a week.

sources:
http://www.fas.org/man//gao/nsiad98001/c1.htm
http://www.gastec.com.my/Hydrogen/H2%20 ... tation.pdf
How you can store hydrogen in a tank intended for storing of jet fuel?

Right, 20 Nm3/h after some altering
This is the link of another company with whom these types of electrolizers are marketed: http://www.ask-technology.ru/production/tech.html
(by the request of customer capacity can be increase to 15-20 m3/h)
d
And nobody can say thanks to what this cappacity increases. I assume that thanks to inrease of working volume. And base capacity is 2,5 nm3/h

Nydoc
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Post by Nydoc »

Joseph Chikva wrote:How you can store hydrogen in a tank intended for storing of jet fuel?
Yes I know :wink:
I would assume the intent was to react it with CO2 before storing it anyway, but my point was with that with these reactors you can create an obscene amount of H2 in a short period of time. It really wouldn't take much space to produce at 100 Nm3/h compared to the space 3.5 million gallons of fuel takes up. A higher production rate would probably be excessive.

KitemanSA
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Location: OlyPen WA

Post by KitemanSA »

Nydoc wrote:
KitemanSA wrote:1500MW power each, given efficiencies. We put that kind of power into carriers now, shock / battle hardened, instant restartable, i.e. EXPENSIVE power now.
Are you sure this is the case?
If you could go back before my edit, you would have seen 750MW rather than 1500. 750 is almost exactly what the Ford class has. When I remembered another efficiency factor, I doubled it. But that just means four reactors instead of two. And besides, I envision LFTRs rather that PWRs so the total size of the power system would still be smaller and lighter(?) than the Ford class power plants.
Nydoc wrote:
Nuclear power plants are simpler and smaller, with reduced maintenance and personnel requirements. ... The nuclear power plant on CVN-21 -- the next-generation carrier now undergoing detailed design in Newport News -- is expected to require only half the manpower than power plants on Nimitz-class ships, the GAO letter to Bartlett said. The yard has also said the electricity that the new power plant creates -- more than 2.5 times the juice of a Nimitz ship -- will translate into many additional manpower reductions throughout the ship.

http://articles.dailypress.com/2006-07- ... t-carriers
A Nimitz class carrier has a maximum propulsion of 260000 bhp. This is about 194 MW, so I would have thought that a Gerald R. Ford class carrier could produce about 485 MW.
The A4W produces ~550MWth iaw Wikipedia. That equates to ~200MWe per plant. Per you quote, this would imply 500MWe per plant, or 1GW overall for the CVN78. But I think your quote applies only to the electrical power part but not the propulsion part of the output. So I'm sticking with about 750MWe total.

Joseph Chikva
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Joined: Sat Apr 02, 2011 4:30 am

Post by Joseph Chikva »

Nydoc wrote:
Joseph Chikva wrote:How you can store hydrogen in a tank intended for storing of jet fuel?
Yes I know :wink:
I would assume the intent was to react it with CO2 before storing it anyway, but my point was with that with these reactors you can create an obscene amount of H2 in a short period of time. It really wouldn't take much space to produce at 100 Nm3/h compared to the space 3.5 million gallons of fuel takes up. A higher production rate would probably be excessive.
I assume you meant "hydrogen reacting with nitrogenium for making NH3" and not "to react it with NH3 before storing".
Design of storage tank for NH3 also differs from tank for storing jet fuel or any other light hydrocarbon (gasoline, diesel fuel). But this is not a problem.

100 Nm3/h of H2 means only 8.93 kg/h = 214.32 kg/day of H2
This corresponds to 1214.48 kg/day of NH3
And this is too low capacity.

Joseph Chikva
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Joined: Sat Apr 02, 2011 4:30 am

Post by Joseph Chikva »

KitemanSA wrote:750 is almost exactly what the Ford class has. When I remembered another efficiency factor, I doubled it.
.........................................................................
So I'm sticking with about 750MWe total.
Stick, stick

What efficiency cruisers and destroyer engines have?
More or less than 50%?

Somebody here asked RATIONAL data and answers. Who was that person? :)

Admit that your idea to make fuel for escort ships onboard of nuclear powered "oiler" is a dead idea.

I advise you to return back to idea to make of only jet fuel, as that can make sense.

KitemanSA
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Location: OlyPen WA

Post by KitemanSA »

Does anyone who can READ have any comments?

Joseph Chikva
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Joined: Sat Apr 02, 2011 4:30 am

Post by Joseph Chikva »

KitemanSA wrote:Does anyone who can READ have any comments?
Do you not can read yourself?

Nydoc
Posts: 40
Joined: Sat Nov 01, 2008 9:45 am

Post by Nydoc »

Joseph Chikva wrote:100 Nm3/h of H2 means only 8.93 kg/h = 214.32 kg/day of H2
This corresponds to 1214.48 kg/day of NH3
And this is too low capacity.
You're right, I had the wrong density written down when I did my conversion. However, suppose you had 90 times this production rate and let's suppose the 20 Nm3/h is reasonable for a 9 cubic meter unit. That would give us about 500 gallons of methane an hour and occupy perhaps 5000 cubic meters. It's still probably on the small side, but it's not that bad of a ratio.

Joseph Chikva
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Joined: Sat Apr 02, 2011 4:30 am

Post by Joseph Chikva »

Nydoc wrote:
Joseph Chikva wrote:100 Nm3/h of H2 means only 8.93 kg/h = 214.32 kg/day of H2
This corresponds to 1214.48 kg/day of NH3
And this is too low capacity.
You're right, I had the wrong density written down when I did my conversion. However, suppose you had 90 times this production rate and let's suppose the 20 Nm3/h is reasonable for a 9 cubic meter unit. It's still probably on the small side, but it's not that bad of a ratio.
Methane?
I heard about two types of process. In both so called "synthesis-gas" the mix of carbon monoxide and hydrogen is used.

First
For producing of methane or higher hydrocarbons you need CO gas to mix with hydrogen, then to maintain certain temperature about 200 C deg and Fischer-Tropsch reactor.
Then to separate hydrocarbons from water and then to distill hydrocarbons.

The second
Only methane is produced by so called "methanization" process widely used in conventional ammonia or pure hydrogen production cycles as final process for avoiding CO pollution into atmosphere.
e.g. http://www.faqs.org/patents/app/20100093525

Both processes are similar to each other but puposes are different and catalysts differ too.
The second process is more selective but gives less valued product (methane).

If you would direct into storage tank a hydrogen, you will not get methane automatically. And saying "That would give us about 500 gallons of methane an hour and occupy perhaps 5000 cubic meters." you are wrong as for this serious hardware is required.

Blankbeard
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Joined: Wed Nov 21, 2012 9:56 pm

Post by Blankbeard »

KitemanSA wrote:
Joseph Chikva wrote:
KitemanSA wrote: So you are telling me you know the reaction NH3 + NOx = N2 + H20 is endothermic?
I know that it does not matter is that reaction exo or end if you execute that reaction in exhaust system. Because even that will be exo, that from exhaust pipe will not make more work, but simply will heat up an environment.
Well DUHH!!!
Reading through this thread I noticed this argument went on (and on) for several pages and never got answered.

NH3 + NO = N2 + H20

Balance it
4NH3 + 6NO = 5N2 + 6H2O

Enthalpy of Formation for each from http://en.wikipedia.org/wiki/List_of_st ... _formation

N2 = 0
NH3 = -27
NO - 80 (Highest of the common oxides i.e. most likely to be endothermic)
H2O = -237

Total of the reactants
-27 * 4 + 80 * 6 = 384

Total of the products
0*5 + -237 *6 = -1422

This reaction is exothermic.

On the issue of size of hydrogen production equipment, I can only offer the observation that a home electrolysis set up is small and rather high rate. Assuming constant current and that we care only about the amount of hydrogen, the weight in ,moles of hydrogen would be equal to the current times the time divided by Faraday's Constant i.e. A*T/(96,485) That's 96 thousand. To produce 1 mole per hour, you'd need 96,485/3600 or approximately 27 amps continuously for one hour. Assuming 110 volts, that's a bit less than 3kw to produce 1 mole of hydrogen.

1 mole of hydrogen weighs about 1kg. In producing it you will produce 1/2 mole of oxygen. The input is 1 mole of water, roughly 9 kg. Water has a volume of about 1 liter per kg (Salt water is a bit more) so let's assume a volume of at least 20 times that so that we don't have to deal with our electrolyte falling out of solution due to volume changes. A single 0.15 inch wire is capable of carrying that current and the whole apparatus will fit in a single cubic meter, exclusive of whatever you use to compress and refrigerate the hydrogen. If you're using the Haber-Bosch process you don't need to cool the hydrogen.

http://www.usni.org/magazines/proceedin ... ndence-oil
This article gives the Navy's oil usage at 33 thousand gallons every ten minutes. That's 198 thousand gallons per hour
This
http://www.energybulletin.net/stories/2 ... nd-figures
says that 75% of the Navy's fuel is used for vehicles. Let's replace that number with ammonia. Ammonia has roughly 1/3 the energy density of diesel and there are about 3.8 liters in a gallon.

Putting all of that together suggests we need to produce 1.7 million liters of ammonia per hour to run the entire Navy. Liquid ammonia weighs about 0.68 kg per liter. One mole of ammonia weighs 17 kg. We need roughly 68 thousand moles of ammonia per hour.

To produce one mole of ammonia takes one mole of N2 and 3 moles of H2 so we need 204 thousand moles of hydrogen per hour. Let's make the assumptions that all of the fuel we are replacing is used by ships or ship based aircraft and that all six fleets use an equal amount of fuel. So we need 34,000 cubic meters of hydrogen production per fleet.

Assuming that 1/8 of the ship's overall volume can be devoted to hydrogen production, that would be around 18,750 cubic meters per ship. So two ships per fleet.

Issues

If I didn't source it, it's probably inaccurate. At least a bit.

Ships volume was calculated from wiki, using waterline dimensions and I didn't attempt to calculate how much of that is superstructure. These ships have more than 1/8 of their volume available for mission, don't they?

Capturing nitrogen from the atmosphere should be compact but you'll need to remove the water vapor (probably) and oxygen. Removing oxygen is easy but what do you burn? You don't want to have to cool that volume of air (1.9 million liters) to a temperature where nitrogen is liquid just to heat it back up again. It's too much to burn. Zeolite, SPA are possible. This
http://humanresearchroadmap.nasa.gov/tasks/?i=801
suggests that a machine producing 4 liters of oxygen would weigh about 8 pounds and consume 106 watts of power. That means it also produces 15 liters of nitrogen per minute. for 1.9 million liters per hour we'd need 36 (No, 2112) of them, consuming about 4 (No, 232) kw and weighing less than 400 pounds (No, less than 17,000 pounds) . That's not what I was expecting.

Edit: Originally, I used a rate of 15 liters per second, not minute. Sorry.

Aircraft range would be a problem. Like 1/3 of current. Needs work.

Storage!!!! Where/how? Replacing diesel with ammonia would be very expensive, I think. Isn't ammonia corrosive to rubber?

Probably other stuff I didn't think of.

Apologies for any errors. Does this sound reasonable?

Joseph Chikva
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Post by Joseph Chikva »

Blankbeard wrote:1 mole of hydrogen weighs about 1kg.?
1 mole of hydrogen weighs 2g. Thanks.

KitemanSA
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Location: OlyPen WA

Post by KitemanSA »

Blankbeard wrote:
KitemanSA wrote:
Joseph Chikva wrote:I know that it does not matter is that reaction exo or end if you execute that reaction in exhaust system. Because even that will be exo, that from exhaust pipe will not make more work, but simply will heat up an environment.
Well DUHH!!!
Reading through this thread I noticed this argument went on (and on) for several pages and never got answered.

NH3 + NO = N2 + H20

This reaction is exothermic.
Thanks. What about with NO2, the other part of NOx?

Blankbeard
Posts: 105
Joined: Wed Nov 21, 2012 9:56 pm

Post by Blankbeard »

KitemanSA wrote: Thanks. What about with NO2, the other part of NOx?
NO2 is listed in the link as 51.3 The higher oxides of nitrogen have smaller and eventually negative enthalpies. I assumed pure NO because that produced the reaction most likely to be endothermic. But it just ain't overcoming that much water as a product.

Blankbeard
Posts: 105
Joined: Wed Nov 21, 2012 9:56 pm

Post by Blankbeard »

Joseph Chikva wrote:
Blankbeard wrote:1 mole of hydrogen weighs about 1kg.?
1 mole of hydrogen weighs 2g. Thanks.
DOH! Of course, you are right. Luckily, I didn't use that figure so it doesn't change the rest of the post.

Something else I thought of. Iron based catalysts have only about a 15% efficiency when run at 400 atm and 400 degrees. That means you have to cycle the gas several times to convert it all. Better plants have lowered the required pressure to only about 80 atm which is safer. The Navy is likely to use the more expensive and much more effective ruthenium catalyst that works at lower pressures with the same efficiency. I'd expect the Navy to use the highest safe pressure with the ruthenium to maximize efficiency. Also, the lower the temperature, the higher the efficiency but the slower the reaction. It's a pickle.

Even then, this is an expensive proposition.

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